Fault of the IR Alignment A320

1. Possible Causes:

-wiring

2. Job Set-up Information

A. Referenced Information

REFERENCEDESIGNATION
Ref. 34-58-00-810-828-AGPS PRIMARY LOST displayed on the NAV DISPLAY
Ref. AMM 34-10-00-860-004IR Alignment Procedure
Ref. AWM 34-11-44
Ref. AMM 34-12-34-000-001Removal of the ADIRU
Ref. AMM 34-12-34-400-001Installation of the ADIRU
Ref. AMM 34-14-00-740-004SYSTEM TEST of the Inertial Reference (IR)

3. Fault Confirmation

SUBTASK 34-12-00-710-050-A

A. Test(s)

(1) Do the IR alignment procedure or the automatic IR-alignment procedure Ref. AMM 34-10-00-860-004:

(a) If the IR alignment is not satisfactory:

— Go to Para. Fault Isolation.

(b) If the IR alignment is satisfactory:

— No maintenance is necessary.

4. Fault Isolation

SUBTASK 34-12-00-810-050-A

A. If the test confirms the fault:

(1) Do the system test of the IR Ref. AMM 34-14-00-740-004:

(a) If the system test gives maintenance message(s):

— Do the related troubleshooting procedure.

(b) If the system test does not give maintenance message(s):

— Continue the troubleshooting.

SUBTASK 34-12-00-810-051-A

B. If the fault continues:

(1) Make sure that you enter the aircraft position (manually or automatically).

(2) Do a check:

— For the ECAM warning(s) NAV IR 1 FAULT and/or NAV IR 2 FAULT and/or NAV IR 3 FAULT, or

— On overhead panel 20VU, on the ADIRS CDU, if the IR1 FAULT and/or IR2 FAULT and/or IR3 FAULT light(s) come on.

(a) If the ECAM warning(s) NAV IR 1 FAULT and/or NAV IR 2 FAULT and/or NAV IR 3 FAULT is (are) shown or if the IR1 FAULT and/or IR2 FAULT and/or IR3 FAULT light(s) is (are) on:

— Replace ADIRU 1 and/or ADIRU 2 and/or ADIRU 3 Ref. AMM 34-12-34-000-001 and Ref. AMM 34-12-34-400-001.

(b) If the ECAM warning(s) NAV IR 1 FAULT and/or NAV IR 2 FAULT and/or NAV IR 3 FAULT is (are) not shown or if the IR1 FAULT and/or IR2 FAULT and/or IR3 FAULT light(s) is (are) off:

— Continue the troubleshooting.

SUBTASK 34-12-00-810-052-A

C. If the fault continues:

(1) On overhead panel 20VU, on the ADIRS CDU, set the IR1, IR2 and IR3 selector switches to the ATT positions for a minimum of five seconds to disable the position comparison test.

(2) Do the IR alignment procedure or the automatic IR-alignment procedure Ref. AMM 34-10-00-860-004:

(a) If the IR alignment is satisfactory:

— No maintenance is necessary.

(b) If the IR alignment is not satisfactory:

— Continue the troubleshooting.

SUBTASK 34-12-00-810-053-A

D. If the fault continues:

(1) On the CAPT ND or the F/O ND, do a check for the message GPS PRIMARY LOST:

(a) If the message GPS PRIMARY LOST is shown, do the troubleshooting procedure Ref. TSM TASK 34-58-00-810-828:

1 If the GPS position is not available:

a On the MCDU, push the DATA mode key (the DATA INDEX page comes into view).

b On the MCDU, on the DATA INDEX page, push the line key adjacent to the GPS MONITOR indication (the GPS MONITOR page comes into view).

c On the MCDU, on the GPS MONITOR page, manually enter the PPOS.

d Do the IR alignment procedure Ref. AMM 34-10-00-860-004.

(b) If the message GPS PRIMARY LOST is not shown:

— Continue the troubleshooting.

SUBTASK 34-12-00-810-054-A

E. If the fault continues:

(1) On the MCDU, push the INIT mode key (the INIT A page comes into view).

(2) On the MCDU, on the INIT A page, push the line key adjacent to the IRS INIT indication (the IRS INIT page comes into view).

(3) In the IRS1 ALIGNING ON GPS and/or IRS2 ALIGNING ON GPS and/or IRS3 ALIGNING ON GPS field(s), do a check to see if the indication(s) is (are) shown as dashes:

(a) If one or more indications is (are) shown as dashes, do a check of the AUTO ALIGN ON GPS function:

1 If the AUTO ALIGN ON GPS function is not activated:

a Manually enter the PPOS.

b Do the IR alignment procedure Ref. AMM 34-10-00-860-004.

2 If the AUTO ALIGN ON GPS function is activated:

a Do a check and repair the wiring of ADIRU 1, ADIRU 2 and ADIRU 3 from pin AB to GND Ref. AWM 34-11-44.

b If the wiring is correct:

— Do the IR alignment procedure or the automatic IR-alignment procedure Ref. AMM 34-10-00-860-004.

c If the wiring is not correct:

— Continue the troubleshooting.

(b) If the indication(s) is (are) not shown as dashes:

— Continue the troubleshooting.

SUBTASK 34-12-00-810-055-A

F. If the fault continues:

(1) Do a check for the indications and the messages that follow:

On the upper ECAM DU, the IR IN ALIGN x MIN or the IR IN ALIGN memo(s) flashes green.

On the MCDU scratchpad, the messages:

— CHECK IRS/AIRPORT POS

— REF/GPS POS DIFF

— REF/LAST IRS POS DIFF

— REALIGN IRS MCDU.

On overhead panel 20VU, on the ADIRS CDU:

— The IR1 ALIGN and/or IR2 ALIGN and/or IR3 ALIGN indication light(s) flash(es).

(a) If one or more of these indication(s) or message(s) is (are) shown:

1 Do one of these steps to enter the correct PPOS:

a On the MCDU:

— Push the INIT mode key (the INIT A page comes into view).

— On the INIT A page, push the key adjacent to the IRS INIT indication (the IRS INIT page comes into view).

— On the IRS INIT page, enter the correct PPOS.

b On overhead panel 20VU, on the ADIRS CDU, enter the correct PPOS as follows:

— If the latitude value is 43°37.4’N, enter N4337.4 in the ADIRS CDU window, then push the ENT key.

— If the longitude value is 1°22.3’E, enter E001223 in the ADIRS CDU window, then push the ENT key.

2 Do the ADIRU alignment procedure Ref. AMM 34-10-00-860-004.

(b) If these indications and the messages are not shown:

— Continue the troubleshooting.

SUBTASK 34-12-00-810-056-A

G. If the fault continues:

(1) On the MCDU and/or the ADIRS CDU, if the message XCESS MOTION is shown:

— Do the IR alignment procedure after you stop the aircraft movement Ref. AMM 34-10-00-860-004.

Read me first

All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

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